JASC 5710
Service difficulty reports · 4,458
Reports filed under 5710 · Wing Main, Frame Structure, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5710' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5710' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2024090314929Support Fitting · crackedL/W REAR SPAR T/E LOWER ACCESS PANEL 551GB I/B FWD SUPPORT RODS UPPER SUPPORT FITTING CRACKED MKD DOT<[01] REMOVED AND REPLACED SUPPORT FITTING P/N 115A2350-1 AT L/W REAR SPAR T/E LOWER ACCESS PANEL 551 GB I/B FWD SUPPORT ROD UPPER AS PER SRM 51-40-02-0G-0; SRSDR IPXA2024082194989Strip · corrodedRIGHT WING OUTBD AILERON LOWER T/E SURFACE A LOT OF PLACE CORROSION & DISCHARGER STATIC & UPPER SURFACE ONE PLACE (REPAIR). I.A.W AMM 20-51-01-912-008 REV.111 INSTALL RH WING OUTBD AILERON LOWER PANEL. CONDITION CHECK NORMAL.SDR IPXA2024082166256Strip · corrodedAGING A/C INSPECTION : FOUND LH WING OUTBD AILERON T/E & DISCHARGE CORROSION. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 INSTALL LH WING OUTBD AILERON LOWER PANEL. CONDITION CHECK NORMAL.SDR IPXA2024082166845Collar · crackedR/H WING STA : OLES 1581 FRONT SPAR SURFACE ONE HI-LOCK COLLAR CRACK (AGING A/C INSPECTION). (REPLACE). INSTALL NEW FASTENER I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO:112U5630 SH.1 REV.A.SDR IPXA2024081564774Rod · corroded**SUPPLEMENTAL SDR** FAULT - R/H WING STA OLES 1483.95 , 1493.45 FRONT SPAR FIXED PNL 2EA SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD. REVIEWEDSDR IPXA2024081564749Link · corrodedR/H WING STA OLES 1525.45 FRONT SPAR FIXED PNL SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.SDR UIEA2024071500678Fitting · corrodedRHW LWR WING L/E COMPOSITE PANEL FOUND BULGED AT OLES 1390(<P>FITTING REPLACED AND INSTALLED AS PER RI-57-21-16994 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024090312246Support Beam · crackedLH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LH WING TE DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM AFT END FITTING ORRS 261+8 IAW SRM 51-10-02-0G-0 PAR 9.A AND SRSDR SWAA2024082212157Beam · corrodedCORROSION TRAILING EDGE BEAM ON TOP LOWER SURFACE BETWEEN ORSS 452 TO ORSS 505 AT RT WING. REPLACED TRAILING EDGE BEAM AND FASTENERS ON TOP LOWER SURFACE BETWEEN ORSS 452 TO ORSS 505 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG: 115A3710 SHEET:SDR SWAA2024082212165Beam · corrodedCORROSION TRAILING EDGE BEAM ON TOP LOWER SURFACE LOCATED BETWEEN ORSS 333 TO ORSS 432 AT RT WING. REJECTION MISSING FASTENERS FASTENER COLLAR APROX ON ORSS 404 AT RT WING (1 EA) SEE TTG8Q00V7UUY. REPLACED TRAILING EDGE SUPPORT BEAM LOCATED BETWEEN ORSS 33SDR SWAA2024082212166Beam · corrodedCORROSION ON BEAM AT TRAILING EDGE BETWEEN ORSS 273 TO ORSS 321 LOWER SURFACE AT RT WING. REPLACED BEAM AND FASTENERS LOCATED ON TRAILING EDGE BETWEEN ORSS 273 TO ORSS 321 LOWER SURFACE AT RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A3SDR NACA2024071200002Structure · corrodedDURING NRC CA1559/206 CORRECTIVE ACTION FOUND CORROSION BETWEEN NO.9 SPOILER OB END RIB AND L/E CHANNEL. REPAIRED CORROSION IAW SRM 57-70-05SDR HNAA2024090400214Torque Box · crackedFOLLOWING NDT INSPECTION, CRACK INDICATION FOUND IN R/H WING TORQUE BOX #1 AT SPAR 3, FORMOST OUTBD INNER HOLE.SDR DALA2024071107028Strut · damagedSHIP 3137 BENT PROXIMITY SENSOR 37CV ON INTERCONNECTING STRUT LH WING. CORRECTIVE ACTION: REPLACED PROXIMITY SENSOR 37CV ON INTERCONNECTING STRUT LH WING AS PER A320 FAM AMM 27-51-44-000- 002-A AND AMM 27-51-44-400-002-A. (0440192)SDR DALA2024071107027Strut · damagedSHIP 3137 TOOL MARK PROXIMITY SENSOR 38CV ON INTERCONNECTING STRUT RH WING. CORRECTIVE ACTION: REPLACED PROXIMITY SENSOR 38CV ON INTERCONNECTING STRUT RH WING AS PER A320 FAM AMM 27-51-44-000- 002-A AND AMM 27-51-44-400-002-A. (0440186)SDR SWAA2024072910082Beam · elongatedLEFT WING TRAILING EDGE INBD FIXED TRAILING EDGE PANEL SUPPORT BEAM (ABOVE DEFLECTION CONTROL RIB) HAS ELONGATED FASTENER HOLES.(MARKED)<[01] PANEL SUPPORT BEAM IS OUT OF LIMITS PER SRM 57-51-02-1A-1. REMOVE AND INSTALL NEW BEAM IN CONJUNCTION WITH NONROUTINE SDR SWAA2024071110063Erosion Shield · delaminated(A150-001) CORNER DELAMINATED ON LEFT WING L/E PANEL 521TB.<[01] BONDED LOOSE EROSION STRIP IAW SRM 57-41-01-2R-6;[02] AUDITSDR UIEA2024070300573Reinforcement · mechanic errorLH WING REINFORCEMENT ANGLE AT STR L-11 BETWEEN RIB 10 AND 11 WITH MIS DRILL HOLES(<P>MIS DRILL HOLES ON REPAIRED LH WING REINFORCEMENT ANGLE AT STR L-11 BETWEEN RIB 10 AND 11 WERE REPAIRED IAW FVCI EO NO. 24097-1 REV. IR. NO FURTHER DEFECTS NOTED.</P>)SDR SWAA2024072909595Support Beam · crackedRT WING T/E; LOWER PANEL 661AB SUPPORT BEAM CRACKED AT I/B END.<[01] REMOVED SUPPORT BEAM AT R/W T/E ON LOWER PANEL 661AB AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW BEAM ASSY AS PER SRM 51-40-05-0G-0. INSTALLED NEW NUT PLATES ON NEW BEAM ASSY AS PER SRMSDR AALA202409032672Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT JACK FITTING BETWEEN WS 070 AND WS 141 BETWEEN RIBS 2 AND 3. REPAIRED LANDING GEAR RETRACTION ACTUATOR ATTACHMENT JACK FITTING PER EA 356779.SDR SWAA2024082609176Vapor Barrier · crackedCRACK ON VAPOR BARRIER LOCATED BS663 LBL52 AND WL160 CENTER WING BOX 2024-420712<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: 15120589 DUE DATE: 13-FEB-24.;[02] CORRECTED STEP 1 TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 07-NOV-24.;[03] TOOL USEDSDR WX0A2024081932157Wing Root · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0005: R/H WING TRAILING EDGE CORROSION FOUND AT WING ROOT OVERWING PANEL BETWEEN INBD JOINT STRIP AND NUT STRIP RETAINERS. / RH WING TRAILING EDGE OVERHANG BETWEEN RIB 1-2SDR FDEA202407020911Former · crackedRIGHT WING - FIXED LEADING EDGE UPPER FORMER AT STATION XOS 673 FOUND CRACK ABOUT 1.2". RIGHT WING FIXED LEADING EDGE UPPER CRACKED FORMER AT STATION XOS 673 REMOVED AS PER SRM 51-31-01-0G. FABRICATED FORMER AS PER DOUGLAS DRAWING ARB 2924 REVISION B. FASDR SWAA2024080507998Winglet · corrodedCORROSION TIP WINGLET AT LT WING 2024-402153<[01] REPAIRED TIP WINGLET AT LT WING IAW AVIATION PARTNERS BOEING 737-NG WINGLET AP37.1-0632 SRM-57-30-01 REPAIR 6 PARAGRAPH 4.A;B. AND C. FIGURE 201 DETAIL 2 SEE I;[02] CORRECTED STEP<BR>REPAIRED TIP WINGLET AT LT SDR SWAA2024070106926Plate · crackedON CLIMBOUT OF DEN GOING THROUGH 27000FT LEFT TANK FUEL FUEL IMBALANCE OF 1400LBS WITHIN 1 MINUTE.<[01] DURING CROSSFEED VALVE ALIGNMENT CHECK; FOUND CROSSFEED VALVE INDEXING PLATE CRACKED. R&R AND REALIGNED INDEXING PLATE PER AMM 28-22-21. OPS CHECK GOOD.SDR DALA2024062806588Strut · corrodedSHIP 3132 CORROSION INTERCONNECTING STRUT INTERNAL AREA ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING AS PER A320 FAM AMM 27 -51-44-000-001-A AND AMM 27-51-44-400-001-A. (0416719)SDR SWIA202409160026Panel · damagedENLARGED HOLES IN AIRFRAME STRUCTURE LH WING PANEL 531AZ (MX 28441519) (C-CHECK RO 9/15/2024) REPAIRED ENLARGED HOLE IN ACFT STRUCTURE AT LH WING PANEL 531AZ PER REO 690-57-42-1095 REV-- DATED 2024-08-08. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITHSDR FDEA202406200820Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER DOUBLER FOUND CRACK AT STATION XOS 789 APPROXIMATELY 0.75 INCH RIGHT FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G.SDR HNAA2024072600576Torque Box · cracked53-2384 RH WING TQ BOX 1 ATTACHMENT TO WING SPAR 1LWR IB HOLE HAD NDT INDICATION. REPAIRED IAW EO1-27-24-0404SDR FDEA202406190819Former · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER FOUND CRACK AT STATION XOS 808 APPROXIMATELY 4 INCH. RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER AT STATION XOS 808 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER SDR FDEA202406190818Former · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT FORMER FOUND CRACK AT STATION XOS 795 APPROXIMATELY 1 INCH RIGHT HAND WING FIXED LEADING EDGE INTERNAL SUPPORT CRACKED FORMER AT STATION XOS 795 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FSDR SWAA2024072511978Plate · looseRIGHT WING DEFLECTOR RIB TO DEFLECTOR PANEL AT SERRATED PLATES LOOSE<[01] ACCOMPLISHED REPAIR AT RIGHT WING DEFLECTOR RIB UPPER TAB IN REF B737-700 SRM 57-51-02-2R-4; VIEW A-A AND 57-51-02-2R-1; VIEW B-B.;[02] VERIFIED STEP 1SDR SWAA2024070501855Winglet · damagedLEFT WINGLET/SCIMITAR WRAP AROUND ACCESS PANEL HAS 1EA ELONGATED HOLE<[01] REPAIRED DAMAGE HOLE AT LAFT WINGLET/SCIMITAR WRAP ACCESS PANEL AS PER SRM 51-70-04-2R-9. MATERIAL USED EA9390 PO #2061896.<BR>PERFORMED ULTRASOUND INSPECTION OF REPAIRED AREA AND MINIMSDR SWAA2024070801602Tee Angle · damagedRIGHT WING TRAILING EDGE PANEL 651GB INBOARD 'T' BRACKET FORWARD BEARING HOLE IS ELONGATED. MARKED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] APPLIED FINISH PER AMM 5SDR COEA2024080227738Fairing · gougedWO 258184 NR 600005 DISCREPANCY: R/H WING STRUT UPPER FORWARD FAIRING GOUGED. CORRECTIVE ACTION: REPAIRED IAW C408 TEXTRON DQ44732M1.SDR COEA2024080224738Fairing · gougedL/H WING STRUT UPPER FORWARD FAIRING GOUGED. CORRECTIVE ACTION: REPAIRED IAW C408 TEXTRON DQ44732M1.SDR DALA2024061406083Structure · corrodedSHIP 3137 CORROSION TRAILING EDGE BETWEEN RIB 7 TO RIB 9 ON LH WING. CORRECTIVE ACTION: REMOVED CORROSION BY REWORK AS PER A319 SRM 51-74-00. (0391805)SDR CALA2024061301795Landing · wornPNEUMATIC ACCESS PANEL 192DR STRUCTURE WHERE OUTBD LATCH ATTACHES WORN. SEE IMAGE. WORK ACCOMPLISHED ON NR 002042281 REPAIR CATEGORY A VERIFIED WORK ACCOMPLISHED ON NR 002042281.SDR SWAA2024062102105Panel · damagedLEFT WING DEFLECTOR CONTROL RIB UPPER COMPOSITE PANEL HAS 4 EACH ELONGATED HOLES AS MARKED<[01] ACCOMPLISHED REPAIR AT LEFT WING DEFLECTOR CONTROL RIB UPPER COMPOSITE PANEL 4 EACH FASTENER HOLES AND TOPCOATED PER SRM 51-70-04-2R-9 AMM 51-21-73-370-803;[02] VERSDR SWAA2024061400643Retainer · crackedLEFT WING DEFLECTION RIB UPPER SHELF PANEL SEAL RETAINER CRACKED.<[01] REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02;[02] C/W INSP.REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02SDR UIEA2024051400389Support · corrodedLHW UPPER FIXED PANEL 511CTA O/B SUPPORT CHORD FOUND CORRODED.(<P>CORRODED AREA BLENDED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLEND OUT AREA MEASURED: L=18" X W=1.6" X D=0.035" WITHIN SRM 57-41-09-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. SDR UIEA2024052300429Spar Web · crackedRHW #3 MAIN TANK MID SPAR WEB AFT FACE BETWEEN WS 382.22 AND WS 411.41 AREA FOUND 2EA FASTENER HOLE CRACK(<P>MID SPAR WEB 2EA FASTENER HOLES CRACK AREA REPAIRED AS PER RI-57-20-16903 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300430Support Beam · corrodedRHW L/E FRONT SPAR CAVITY LOWER FIXED PANEL FWD SECTION SUPPORT BEAM FOUND CORROSION AT ILES 480 (#15 KRUEGER FLAP AREA)(<P>SUPPORT BEAM REPAIRED AS PER RI NO. RI-57-41-16871 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR IPXA2024070300970Fitting · crackedCRACK FOUND IN FIRST LAYER OF L/W FR40 LOWER RADIUS HOLE. INSTALLED FILLER AND COVER PLATE AT FR40 LH LOWER RADIUS HOLE. WITH BOLT P/N: EN6115V8-24. BTCH: 4297160. NUT P/N: NAS1726-8E. BTCH: 4249205. BOLT P/N: EN6115V5-24, BTCH: 4274797. NUT P/N: NAS1726-5E. BSDR IXXA20240611001Splice · corrodedLH WING, WING SIDE OF BODY SPLICE, UPPER SPLICE EVIDENCE OF CORRION BS 900 TO BS 940.SDR DALA2024061105984Doubler · damagedRT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 3 SHT 1. PERFORMED HFEC IAW B717 PER B717 SRM 57-40-01-2R PROCEDURE 3 AND SDR U2RA2024081500034Structure · corrodedWHILE PERFOMING C CHECK IN GMF FOUND CORROSION ON LH WING L/E CHORD OLES 1530. THIS REPAIR IS CATEGORY A. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-41-13 REPAIR 1 & 51-70-11 (REV 59 20FEB 2024)SDR SWAA2024060397447Panel · crackedRH WING UPPER FIXED TE PANEL 651ET LATERAL STIFFNER CRACKED 12.<[01] UPPER RIGHT WING PANEL (651CT) CRACK IS LOCATED IN THE RADIUS OF THE PANEL STIFFENER JUST FORWARD OF THE VISIBLE NUT PLATES AND IS APPROXIMATELY 12? IN LENGTH. REMOVED AND REPLACED WING PANESDR SWAA2024061902102Retainer · crackedLEFT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] INSTALLED L LOWER HORIZONTAL SEAL RETAINER ANGLE AT LEFT WING O/B DEFLECTION CONTROL RIB PANEL AS PER BOEING 737-800 SRM 51-40-02-0G-0 USED TOOL B/C 173324;[02] REMOVESDR SWAA2024071690667Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING 2024-345621<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 115A3700 SHEET: 41 REV: - TOOL USED DIGITAL CA
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